ASTM E1556-2012 Standard Specification for Epoxy Resin System for Composite Skin Honeycomb Sandwich Panel Repair《合成革 蜂窝状夹层板修补用环氧树脂系统的标准规范》.pdf
《ASTM E1556-2012 Standard Specification for Epoxy Resin System for Composite Skin Honeycomb Sandwich Panel Repair《合成革 蜂窝状夹层板修补用环氧树脂系统的标准规范》.pdf》由会员分享,可在线阅读,更多相关《ASTM E1556-2012 Standard Specification for Epoxy Resin System for Composite Skin Honeycomb Sandwich Panel Repair《合成革 蜂窝状夹层板修补用环氧树脂系统的标准规范》.pdf(9页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: E1556 12Standard Specification forEpoxy Resin System for Composite Skin, HoneycombSandwich Panel Repair1This standard is issued under the fixed designation E1556; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the yea
2、r of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon () indicates an editorial change since the last revision or reapproval.This standard has been approved for use by agencies of the Department of Defense.1. Scope1.1 This specification covers the re
3、quirements for an epoxyresin system intended for the repair of sandwich panels fordurable, rigidwall, relocatable structures. It must be usable in afield environment and shall not require the use of specialequipment such as autoclaves or presses. The epoxy systemcovered by this specification shall b
4、e usable for simultaneousimpregnation of a wet-layup composite skin and bonding ofthat skin to a substrate honeycomb core. The material shallwithstand exposure to temperatures from 54 to 93C (65 to199F) and high relative humidity, and also the combination ofstress, temperature, and relative humidity
5、 that are expected tobe encountered in service.1.2 The values stated in SI units are to be regarded asstandard where only SI units are given or where SI units aregiven first followed by inch-pound units; where inch-poundunits are given first followed by SI units, the inch-pound unitsare to be regard
6、ed as the standard.1.3 The following safety hazards caveat refers only to thetest methods described in this specification. This standard doesnot purport to address all of the safety concerns, if any,associated with its use. It is the responsibility of the user of thisstandard to establish appropriat
7、e safety and health practicesand determine the applicability of regulatory limitations priorto use.2. Referenced Documents2.1 ASTM Standards:2C297/C297M Test Method for Flatwise Tensile Strength ofSandwich ConstructionsD792 Test Methods for Density and Specific Gravity (Rela-tive Density) of Plastic
8、s by DisplacementD2344/D2344M Test Method for Short-Beam Strength ofPolymer Matrix Composite Materials andTheir LaminatesD2584 Test Method for Ignition Loss of Cured ReinforcedResinsD2734 Test Methods for Void Content of Reinforced PlasticsD3165 Test Method for Strength Properties of Adhesives inShe
9、ar by Tension Loading of Single-Lap-Joint LaminatedAssembliesE631 Terminology of Building ConstructionsE1091 Specification for Nonmetallic Honeycomb Core forUse in Shelter PanelsE1749 Terminology Relating to Rigid Wall RelocatableShelters2.2 Military Specifications:3MIL-I-24768 Insulation, Plastic,
10、Laminated, Thermosetting,Glass-Cloth, Epoxy-Resin2.3 Military Standards:3MIL-STD-129 Military Marking for Shipping and StorageMIL-STD-1916 DOD Preferred Methods for Acceptance ofProduct2.4 Commercial Standards:4SAE-AMS-C-9084 Cloth, Glass, Finished for Epoxy ResinLaminates3. Terminology3.1 Definitio
11、nsSee Terminologies E631 and E1749 fordefinitions of general terms used in this specification.4. Physical Requirements4.1 Working Characteristics:4.1.1 ApplicationThe components of the epoxy resin shallbe readily hand-mixed to a smooth consistency suitable forapplication. It shall be uniform and fre
12、e of lumps. The resincomponents, once mixed, shall not settle out. The epoxy1This specification is under the jurisdiction of ASTM Committee E06 onPerformance of Buildings and is the direct responsibility of Subcommittee E06.53on Materials and Processes for Durable Rigidwall Relocatable Structures.Cu
13、rrent edition approved Nov. 1, 2012. Published December 2012. Originallyapproved in 1993. Last previous edition approved in 2008 as E1556 08. DOI:10.1520/E1556-12.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book
14、 of ASTMStandards volume information, refer to the standards Document Summary page onthe ASTM website.3Available from Standardization Documents Order Desk, DODSSP, Bldg. 4,Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098, http:/www.dodssp.daps.mil.4Available from Society of Automotive Engine
15、ers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-0001, http:/www.sae.org.Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States1material shall be suitable for the wet-layup impregnation ofSAE-AMS-C-9084 glass cloth and for application to
16、 corematerials over the temperature range of 16 to 38C (60 to100F) and at relative humidities of 30 to 75 %.4.1.2 Application LifeThe application life of a 200-g kit ofthe mixed epoxy system shall be at least 60 min when tested inaccordance with 4.1.5. The epoxy shall be considered to havereached th
17、e end of its application life when the viscosity of this200-g quantity of mixed adhesive exceeds 20 000 centipoise.4.1.3 CuringThe epoxy system shall be capable of curingat 23 6 2C (73 6 4F) in 7 days, or for no longer than3hata temperature of 60 to 66C (140 to 151F), with a curingpressure not to ex
18、ceed 14 psig. In a 236 3C cure, the curingpressure is not required to be maintained after the first 24 h. Ina236 2C cure, the epoxy material shall develop the propertylevels listed in Table 1 within the first 24 h of cure (see 8.3.5).In order to meet the requirements of this specification, theproper
19、ty levels listed in Tables 2-4 must be achieved with the7-day cure at 23 6 2C (73 6 4F).4.1.4 Storage LifeThe storage life period of the two partsof the epoxy resin system, when stored in airtight containers at23C (73F), shall be at least 12 months from the date ofshipment when tested in accordance
20、with 8.3.5.4.1.5 ViscosityThe viscosity of a 200-g kit of the mixedresin system shall be determined at 23 6 2C (73 6 4F) usinga Brookfield viscometer with a No. 3 spindle at 20 rpm. Aviscosity curve shall be determined by taking a readingimmediately after mixing, and every 5 min thereafter until the
21、viscosity exceeds 20 000 centipoise.The viscosity immediatelyafter mixing shall not exceed 14 000 centipoise.4.2 Mechanical PropertiesMechanical properties of testspecimens prepared and tested as specified in Section 8 shallmeet the respective requirements listed in Tables 2-4.4.3 Instruction SheetT
22、he manufacturer shall provide adated, coded, and titled instruction sheet outlining instructionsfor use of the epoxy system in impregnating and bondingSAE-AMS-C-9084 glass composite skins to honeycomb cores(Specification E1091, Types I or II). These instructions shall besupplied by the manufacturer
23、with the test report whenrequesting qualification (see 7.3) and also with each shipmentof epoxy material (see 10.2). The following information shallbe included:4.3.1 All of the information listed in 6.3.1-6.3.11.4.3.2 The application life of the mixed epoxy system at 236 2C (73 6 4F) and 38 6 2C (10
24、0 6 4F).4.3.3 Mixing instructions shall be stated in detail for theepoxy resin system in the particular container supplied.4.3.4 Application, impregnating, and curing instructions,including the spreading method, thickness range, andtemperature/relative humidity working limitations.4.3.5 Material Saf
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